The list of orbital rocket engines.
Country of origin
Name of company designed this engine
Vehicle name where it is used
Location in the vehicle. Could be "Upper" for upper stage, "1st" for first stage, "2nd" for second stage & etc
Rocket propellant is a material used either directly by a rocket as the reaction mass that is ejected, typically with very high speed, from a rocket engine to produce thrust
Specific impulse is a measure of how effectively a rocket uses propellant or jet engine uses fuel. Measured in seconds
Measured in newtons
Mass in kilogram
Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a rocket, jet engine, propeller engine, or a vehicle propelled by such an engine that indicates the performance of the engine or vehicle.
Pressure in rocker chamber. Measure in "bar"
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